Zobrazeno 1 - 10
of 42
pro vyhledávání: '"D. A. Tuchin"'
Publikováno v:
Solar System Research. 56:461-469
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cce725110d09a362cdca364ddccec3aa
https://doi.org/10.1134/s0038094622070176
https://doi.org/10.1134/s0038094622070176
Publikováno v:
Doklady Physics. 66:333-335
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a912f0a83727bef700a5fb51c095f864
https://doi.org/10.1134/s1028335821120053
https://doi.org/10.1134/s1028335821120053
Autor:
Andrey Georgievich Tuchin, Yury Filippovich Golubev, Victor Vladimirovich Korianov, D. A. Tuchin, A. V. Grushevskii
Publikováno v:
Keldysh Institute Preprints. :1-26
As a result of the analysis of various restrictions on the gravity assists maneuvers (GM) conduction, the generalized estimates of near-planetary regions sizes, the “perturbation rings”, are conducted, in which GM realization for the arbitrary ce
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4b1f5e6301a52f6f4c1266e03e752ca
https://doi.org/10.20948/prepr-2021-2
https://doi.org/10.20948/prepr-2021-2
Publikováno v:
Cosmic Research. 58:277-284
This paper shows that the standard and cumbersome method of traditional justification of constancy of an asymptotic velocity in gravity assists, in the model of the circular restricted three-body problem (RTBP), which is applied in the modern astrody
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1a214e8c840a52b472002e194aa6756d
https://doi.org/10.1134/s0010952520040061
https://doi.org/10.1134/s0010952520040061
Autor:
D. A. Tuchin, Yu. F. Golubev, Sergey Mikhailovich Lavrenov, Andrey Georgievich Tuchin, A. V. Grushevskii, V. V. Koryanov
Publikováno v:
Solar System Research. 54:318-328
We consider space expeditions with a long-term spacecraft stay near the studied celestial body (artificial satellites of small bodies of the Solar System), or expeditions with a possible spacecraft landing on the surface of the celestial body (for ex
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8772592e563128b1e1113708bc4c10af
https://doi.org/10.1134/s0038094620040061
https://doi.org/10.1134/s0038094620040061
Autor:
D. A. Tuchin
Publikováno v:
Journal of Computer and Systems Sciences International. 59:430-450
Methods and algorithms for determining the orbit of a space vehicle onboard using the measurements of global navigation satellite (NS) systems are considered. Methods and algorithms for obtaining radio navigation measurements in the case of the highl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8463576082c7a44bc6e11dc539d58896
https://doi.org/10.1134/s1064230720020112
https://doi.org/10.1134/s1064230720020112
Publikováno v:
Mathematica Montisnigri. 49:87-95
An effective space exploration is impossible without gravity assists (GA) using. Their application relaxes the constraints imposed on the space mission scenarios by the characteristic velocity budgets being realized at the current stage of developmen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c322f169ea95f611e6c90c4acbdc7c75
https://doi.org/10.20948/mathmontis-2020-49-7
https://doi.org/10.20948/mathmontis-2020-49-7
Autor:
Irina Petrovna Kiseleva, A. V. Grushevskii, D. A. Tuchin, Yu. F. Golubev, V. V. Koryanov, Andrey Georgievich Tuchin
Publikováno v:
Solar System Research. 53:473-480
In the context of the circular restricted three-body problem (RTBP), the search for the spacecraft’s asymptotic velocity $${{V}_{\infty }}$$ for gravity assist maneuvers (GMs) can be performed using the Jacobi integral $$J$$ and the main property o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00cb254b8e8228cb255b56bb1d709382
https://doi.org/10.1134/s0038094619060029
https://doi.org/10.1134/s0038094619060029
Publikováno v:
Solar System Research. 53:245-253
Venus, the closest planetary neighbor of the Earth in the Solar System, is eminently suitable for performing gravity assist maneuvers by a spacecraft for a low-cost change of its orbit inclination relative to the ecliptic. We calculate the resonance
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7d54bac9b5c5413c81e85ff4c3cea23b
https://doi.org/10.1134/s0038094619040038
https://doi.org/10.1134/s0038094619040038
Publikováno v:
Доклады Академии наук. 484:281-284
An adaptive, semi‑analytical, and geometrically clear method for synthesis of sequences of Venusian gravity‑assist maneuvers setting the desired inclination of a spacecraft orbit is proposed. The geometric constraint on the maximum possible incli
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c713a0224b24f374127ee58985cad1c3
https://doi.org/10.31857/s0869-56524843281-284
https://doi.org/10.31857/s0869-56524843281-284